Title:
FLIGHT BODY CONTROL SYSTEM AND FLIGHT BODY
Document Type and Number:
Japanese Patent JP2018190024
Kind Code:
A
Abstract:
PROBLEM TO BE SOLVED: To efficiently control a yaw-angle of a flight body.SOLUTION: A flight body control system 100 includes a flight body 1 and a control device 5. The control device 5 controls an attitude angle of the flight body 1. The flight body 1 includes a first rotor group 11 and a second rotor group 12. The first rotor group 11 includes three or more rotors. The second rotor group 12 includes two or more rotors. The first rotor group 11 generates a thrust in a first direction D1. The second rotor group 12 generates a thrust in a direction crossing the first direction D1 so that a torque arm R2 of torque acting the flight body 1 becomes not shorter than a prescribed length.SELECTED DRAWING: Figure 1
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Inventors:
IMAZU ATSUSHI
Application Number:
JP2017089508A
Publication Date:
November 29, 2018
Filing Date:
April 28, 2017
Export Citation:
Assignee:
UNIV OSAKA CITY
International Classes:
G05D1/08; A62C27/00; B64C13/18; B64F3/02
Domestic Patent References:
| JP2014169038A | 2014-09-18 |
Foreign References:
| CN102114914A | 2011-07-06 | |||
| WO2016121008A1 | 2016-08-04 |
Attorney, Agent or Firm:
Hiroyuki Maei